View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60407U 26145.17243522 +.00000000 +00000-0 +13334-4 0 00002
2 60407 53.1599 69.3543 0001003 89.2989 270.8144 15.69709201 06
| Epoch (UTC): | 25 May 2026 04:08:18 |
| Eccentricity: | 0.0001003 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 69.3543° |
| argument of perigee: | 89.2989° |
| revolutions per day: | 15.69709201 |
| mean anomaly at epoch: | 270.8144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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